Rolled-up wake field behind aircraft configurations

Vasantha, R (1994) Rolled-up wake field behind aircraft configurations. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    Abstract

    The panel code which accounts for the effects of13; wake behind aircraft configurations has been made13; the new CONVEX super computer of GM MACS .the rolled up operational on DLR aircraft configuration result.. are reproduced and are shown in Figs. I and 2. Using the present panel code results for LTA with rolled-up wake field for different angles of attack and are presented in this report .Vl aircraft are obtained and are presented in this report.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Panel method;Aircraft wake;Wake relaxation;Trailing vorticies
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mr. N A
    Date Deposited: 02 Jun 2006
    Last Modified: 24 May 2010 09:42
    URI: http://nal-ir.nal.res.in/id/eprint/1526

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